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United States Patent | 5,145,319 |
Glowacki | September 8, 1992 |
An axial flow turbomachine rotor comprises a disc having a plurality of annular flanges extending outwardly from its periphery, a plurality of blades secured to the disc and extending radially outwardly from the periphery thereof, each of the blades having its root notched to define heels which are received in the grooves formed between the annular flanges of the disc, and a plurality of separate platforms which are secured to the disc and are disposed between the blades to define the inner boundary of the fluid flow path through the rotor, the blades each being fixed to the disc by two parallel pins which are equidistance from the axis of the disc and are received in corresponding bores passing through the annular flanges and the heels of the blade, the pins also serving to secure the platforms to the disc.
Inventors: | Glowacki; Pierre A. (Fontaine le Port, FR) |
Assignee: | Societe Nationale d'Etude et de Construction de Moteurs d'Aviations (Paris, FR) |
Appl. No.: | 616594 |
Filed: | November 21, 1990 |
Nov 22, 1989[FR] | 89 15301 |
Current U.S. Class: | 416/193A; 416/217; 416/230 |
Intern'l Class: | F01D 005/22; F01D 005/30 |
Field of Search: | 416/193 A,204 A,212 A,214 A,215,217,219 R,220 R,230 |
2326145 | Aug., 1943 | Kroon. | |
2514408 | Jul., 1950 | Mierley. | |
2928653 | Mar., 1960 | Robertson. | |
2999668 | Sep., 1961 | Howald et al. | 416/217. |
3694104 | Sep., 1972 | Erwin. | |
3860361 | Nov., 1975 | McMurtry et al. | 416/212. |
4361416 | Nov., 1982 | Rossmann. | |
4460316 | Jul., 1984 | Partington. | |
4621979 | Nov., 1986 | Zipps et al. | 416/193. |
4696623 | Sep., 1987 | Bost | 416/230. |
Foreign Patent Documents | |||
958441 | Mar., 1950 | FR. | |
989556 | Sep., 1951 | FR | 416/193. |
1234275 | Oct., 1960 | FR. | |
1457941 | Nov., 1966 | FR. | |
2283308 | Mar., 1976 | FR. | |
242977 | Jan., 1926 | GB. | |
619913 | Mar., 1949 | GB | 416/215. |
1331209 | Sep., 1973 | GB. |